Commonwealth legislation

AD/CF34/20 - Critical Time Limited Parts

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This Airworthiness Directive requires operators of General Electric CF34-8C1 turbofan engines to follow the actions set out in FAA AD 2002-23-02 for critical time‑limited rotating parts, with compliance set out in the Requirement Document and an effective date of 31 October 2010. It is intended to prevent failure of life‑limited rotating parts that could cause an uncontained engine failure and aircraft damage. Practically, engine owners/operators and approved maintenance organisations must carry out the inspections, replacements or other actions specified and bear the associated costs and scheduling burdens.

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Current sections

Direct links to the current provisions in AD/CF34/20 - Critical Time Limited Parts.

General Electric Turbine Engines - CF34

General Electric Turbine Engines - CF34 Series

AD/CF34/20	Critical Time Limited Parts	20/2010

Applicability:	General Electric Company CF34-8C1 turbofan engines.
Requirement:	Unless already accomplished, action in accordance with the requirements of FAA AD 2002-23-02.
Compliance:	As specified in the Requirement Document with a revised effective date of31 October 2010.
	This Airworthiness Directive becomes effective on 31 October 2010.
Background:	This AD is issued to prevent critical life limited rotating engine part failure which could result in an uncontained engine failure and damage to the aircraft.

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Mike Higgins
Delegate of the Civil Aviation Safety Authority

5 October 2010

AD/CF34/20

Critical Time Limited Parts

20/2010

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

General Electric Turbine Engines - CF34 General Electric Turbine Engines - CF34 Series

General Electric Turbine Engines - CF34 Series

AD/CF34/20	Critical Time Limited Parts	20/2010

Applicability:	General Electric Company CF34-8C1 turbofan engines.
Requirement:	Unless already accomplished, action in accordance with the requirements of FAA AD 2002-23-02.
Compliance:	As specified in the Requirement Document with a revised effective date of31 October 2010.
	This Airworthiness Directive becomes effective on 31 October 2010.
Background:	This AD is issued to prevent critical life limited rotating engine part failure which could result in an uncontained engine failure and damage to the aircraft.

AD/CF34/20 - Critical Time Limited Parts

Plain English Summary

Deep dive

Current sections

General Electric Turbine Engines - CF34 Series

General Electric Turbine Engines - CF34 Series

AD/CF34/20

AD/CF34/20

Critical Time Limited Parts

Critical Time Limited Parts

20/2010

20/2010

Source text

General Electric Turbine Engines - CF34 General Electric Turbine Engines - CF34 Series

General Electric Turbine Engines - CF34 Series

AD/CF34/20 AD/CF34/20

AD/CF34/20

Critical Time Limited Parts Critical Time Limited Parts

Critical Time Limited Parts

20/2010 20/2010

20/2010